All electric piezoelectric finger sensor (PEFS) for soft material stiffness measurement

ABSTRACT

A PEFS (Piezoelectric Finger Sensor) acts as an “electronic finger” capable of accurately and non-destructively measuring both the Young&#39;s compression modulus and shear modulus of tissues with gentle touches to the surface. The PEFS measures both the Young&#39;s compression modulus and shear modulus variations in tissue generating a less than one-millimeter spatial resolution up to a depth of several centimeters. This offers great potential for in-vivo early detection of diseases. A portable hand-held device is also disclosed. The PEF offers superior sensitivity.

This application is a divisional of U.S. patent application Ser. No. 12/328,639, filed on Dec. 4, 2008, which, in turn, is a divisional of U.S. patent application Ser. No. 11/136,173, filed on May, 24, 2005, now U.S. Pat. No. 7,497,133, which, in turn, is a non-provisional of U.S. Provisional Application No. 60/573,869, filed May 24, 2004, the entire disclosures of which are hereby incorporated by reference as if set forth fully herein.

STATEMENT OF GOVERNMENT INTEREST

This invention was reduced to practice with Government support under Grant No. R01 EB00720-01 awarded by NIH; the Government is therefore entitled to certain rights to this invention.

BACKGROUND OF THE INVENTION

1. Field of Invention

The present invention relates to a piezoelectric sensor for measuring shear and compression.

2. Brief Description of the Prior Art

A typical soft-material/tissue mechanical property tester requires an external force (displacement) applicator and an external displacement (force) gauge.^(1,2) The external force (displacement) generator may be hydraulic or piezoelectric and the external displacement gauge (force gauge) may be optical or piezoelectric. Regardless of the mechanism of force/displacement generation and displacement/force detection, typical tissue/soft-material mechanical testing is destructive and it requires specimens cut to a disc shape to fit in the tester. In addition, a compressive elastic modulus tester e.g., an Instron is also different from a shear modulus tester, e.g., a rheometer.³ Currently, no single instrument measures both the compressive Young's modulus and the shear modulus.

Over the past decades, many techniques have been developed to image tissue structures.⁴⁻⁹ Computer Tomography (CT)¹⁰ takes 360 degree X-ray pictures and reconstructs 3D tissue structures using computer software. Magnetic Resonance Imaging (MRI)¹¹ uses powerful magnetic fields and radio waves to create tissue images for diagnosis. Ultrasound (US)¹² transmits high-frequency waves through tissue and captures the echoes to image tissue structures. T-scan (TS)¹³ measures low-level bioelectric currents to produce real-time images of electrical impedance properties of tissues. Ultrasound elastography (UE)¹⁴ evaluates the echo time through tissues under a constant mechanical stress and compares it to that of the same tissue when unstressed. A tissue strain map is then obtained, from which an image of 2D elastic modulus distribution is created by inversion techniques. Tactile imaging tools using array pressure sensors probe spatial tissue stiffness variations. However none of these techniques have the ability to probe tumor interface properties.

The detection of abnormal tissue as cancerous growth requires improvements in screening technologies. The key to successful treatment lies in early detection. Imaging techniques such as mammography in breast cancer screening, detect abnormal tissue by tissue density contrast. Mammography is the only FDA approved breast cancer screening technique, which has a typical sensitivity of 85% that decreases to 65% in radiodense breasts.¹⁰ However, in these screening processes there is a high incidence of false positives. In fact, only about 15-30% of breast biopsies yield a diagnosis of malignancy. Changes in tissue stiffness have increasingly become an important characteristic in disease diagnosis. It is known that breast cancers are calcified tissues that are more than seven times stiffer than normal breast tissues.¹¹⁻¹⁴ Thus, contrasting levels of stiffness within the breast may indicate cancerous tissue. Similarly, plaque-lined blood vessels are also stiffer than normal, healthy blood vessels.

The examining physician may detect abnormal tissue stiffness by palpation by taking advantage of the fact that cancerous tissues are stiffer than surrounding normal tissues under compression. Thus, palpation has been a useful tool for experienced physicians to diagnose breast and prostate cancer. However, palpation is not quantitative and depends solely on the experience of the individual physician. So there remains a critical need to improve cancer-screening technology to reduce the number of unnecessary biopsies.

SUMMARY OF THE INVENTION

In a first aspect, the invention relates to a sensor for measuring a compression modulus and a shear modulus that has a first layer made of piezoelectric material, a second layer made of a non-piezoelectric material, a first electrode placed on top of the first layer for sensing a displacement of the first layer; and a second electrode placed on top of the first layer for providing a force to the first layer.

In a second aspect of the invention a sensor for measuring a compression modulus and a shear modulus is provided having a first layer made of piezoelectric material for providing a force, a second layer made of non-piezoelectric material, and a third layer made of piezoelectric material for sensing a displacement.

In a third aspect of the invention a method for measuring a compression modulus and a shear modulus is provided. The method has the steps of providing a plurality of sensors made of a piezoelectric material and a non-piezoelectric material at a target, applying a force with at least one of the plurality of sensors, detecting a displacement with at least one of the plurality of sensors, and providing a measurement of a compression modulus and a shear modulus of said target.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a schematic of two PZT/stainless steel cantilevers with (a) driving and sensing electrodes both on the top side and (b) with a bottom sensing PZT layer.

FIG. 2 shows a graph of (a) the displacement signals captured by the sensing PZT layer, and (b) the deflection signal captured by the sensing PZT layer.

FIG. 3 shows a graph of peak and displacement measurements.

FIG. 4 shows a representation and schematic of the compression indentation tests.

FIG. 5 shows (a) a regular compression test where the contact area is the same as the surface area, and (b) deformation of a sample in a regular compression test under an applied voltage, V.

FIG. 6 shows a comparison of the elastic modulus obtained in a regular compression test and an indentation compression test.

FIG. 7 shows (a) a 3-D plot of raw elastic modulus data from indentation tests, (b) the corresponding contour plot, (c) smoothed data, to create an enhanced image, and (d) a representation of the simulated tissue.

FIG. 8 shows graphs of the elastic modulus profile of (a) 7 mm diameter wax in gelatin at various depth measured with a 3 mm wide cantilever, (b) 15 mm diameter wax in gelatin measured with a 5 mm wide cantilever, and (c) summary of the detection depth limit of 3 mm wide cantilever and 5 mm wide cantilever.

FIG. 9 shows a schematic of a regular shear test using an L-shaped cantilever where the contact area is the same as the sample surface area.

FIG. 10 shows a schematic of an indentation shear test using an L-shaped cantilever where the contact area is much smaller than the sample surface area.

FIG. 11 shows schematics of (a) regular compression, (b) indentation compression, (c) regular shear, and (d) indentation shear measurements using a cantilever that has a U-shaped stainless steel tip. FIG. 11 e shows a protected version of the cantilever of FIGS. 11 a-11 d designed for measurements in tight spaces.

FIG. 12 shows a graph of the results of regular compression, indentation compression, regular shear, and indentation shear measurements on rubber samples that had a young's modulus 400-500 kPa using the U-shaped cantilever as shown in FIG. 11.

FIG. 13 shows a representation of model tumors and surrounding tissue.

FIG. 14 shows a graphical representation of Young's modulus and shear modulus tests measured by indentation compression and indentation shear tests on various materials.

FIG. 15 shows a graph of a lateral elastic modulus profile of a lumpectomy sample.

FIG. 16 shows (a) a graph of Young's modulus (E) and shear modulus (G) profiles, and (b) G/E profile on breast tissue with cancer.

FIG. 17 shows a graph of elastic modulus, E, profiles measured using an 8 mm wide PEF (open squares) and a 4 mm wide PEF (open squares) on a 15 mm diameter clay inclusion in gelatin.

FIG. 18 shows a representation of a direct tumor mobility measurement made on a model rough inclusion (front) and on a model smooth inclusion (back) in gelatin using two PEFs.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT(S)

A “PEFS” includes a piezoelectric layer bonded to a non-piezoelectric layer to form a cantilever. FIG. 1 a shows a schematic of a lead zirconate titanate (PZT)/stainless steel cantilever with both the driving and sensing electrodes on the top side. FIG. 1 b shows a PZT/stainless steel cantilever with a bottom PZT sensing layer. In these schematics, the PZT represents the piezoelectric layer and the stainless steel represents the non-piezoelectric layer.

In a first aspect of the invention, the PEFS is capable of simultaneously applying a force and detecting the corresponding displacement. The application of a voltage at the driving electrode generates the force and the corresponding displacement is measured by detecting the induced piezoelectric voltage within the sensing electrode. The PEFS can measure both the compressive Young's modulus and the shear modulus of a soft material through the cantilevered tip. Thus, in an aspect of the current invention, the PEFS measures both the compressive Young's modulus and shear modulus using one single device, while at the same time increasing the sensitivity and accuracy of the measurements, relative to some commercially available devices used for this purpose. Comparisons between the shear and compressive measurements using one single device provide clear and accurate information about the interfaces between hard inclusions (tumors) and the surrounding tissue that otherwise could likely not be obtained.

In another aspect of the invention, several PEFS can form an array to measure lateral and in-depth stiffness variations in soft-materials and tissues both under compression and under shear. This ability to self-excite via the driving voltage and self-detect via the sensing electrode allows a PEFS to measure the elastic and shear properties of specimens having complex shapes.

In another aspect of the invention, the PEFS may apply forces and measure displacements at the same time, allowing the device to function using completely electrical means for tissue-stiffness imaging, cancer and disease detection. Thus, the PEFS may be powered with a DC power source allowing the PEFS to take electrical measurements in the DC mode. In this aspect of the invention the PEFS may be part of a portable hand-held device for measuring tissue. This simple all-electrical measurement makes the PEFS look and work like a finger, which may allow for in vivo measurements in tight spaces.

While the sensitivity of the PEFS has been improved by the increased sensitivity of the compression tests with the addition of the shear test to the PEFS, the reduction of the probe size as compared to the bulkiness of current tactile cancer-imaging devices, provides increased versatility as well. In particular, the finger-like shape of the PEFS is now suitable for, for example, prostate cancer detection.

In another aspect of the invention, the PEFS can analyze measurements of various widths allowing the direct experimental determination of a stiffness variation in the thickness direction. Current tumor imaging techniques are incapable of directly measuring a tumor size or position. Instead, these techniques measure the surface mechanical response. The tumor information is generated numerically by the “inversion” technique and used to reconstruct the tumor size and position.^(15,16)

In another aspect of the invention, the PEFS can assess vertical stiffness variations of soft materials/tissues up to several centimeters in depth with increased resolution by use of an array of PEFS's of varying probe widths ranging from less than 1 mm to several cm. Detection of tissue stiffness both under shear and under compression will allow comparison of the stiffness of a hard inclusion such as a tumor, with the stiffness of surrounding normal tissue, not only under compression, but also under shear. Such comparisons will permit a determination of the interfacial properties between the hard inclusion and surrounding tissue, which has the potential to greatly enhance the ability to assess tumor malignancy.

The PEFS is capable of detecting soft-material/stiffness variations in both the shear and the compression modes while under DC power. This allows a portable hand held device to detect soft material/tissue stiffness. Additional advantages result from the ultra-small strains employed for detection (smaller than 1%), and the minimal discomfort that such strains will cause to the patient.

In another aspect of the invention, the PEFS may be fabricated in a variety of shapes including L-shaped, U-L-shaped, U-shaped, square-shaped, O-shaped, tapered, etc. as well as in various lengths and widths. When the PEFS has an L-shaped tip, the PEFS is capable of accurately measuring the shear modulus of soft tissues and materials at very small strain (<0.1%), a capability most of the current commercial rheological instruments lack.

In addition to detection and mapping of a tumor, the PEFS may also be employed as a tissue/soft-material mechanical tester, for breast cancer detection, for prostate cancer detection, for monitoring skin cancer and skin elasticity testing, or for cellular elasticity/plasticity measurements using a miniaturized PEFS. Of course, the PEFS is capable of use in conventional methods for making compression and shear measurements on pliable materials of any kind and its use need not be limited to tissue measurements.

All-electrical measurement. When a voltage is applied to the top PZT layer of a PEFS as shown in FIG. 1( b), it causes the PEFS to bend due to the converse piezoelectric effect, which generates a force, and therefore, a displacement at the cantilever tip. The bending of the cantilever generates an induced piezoelectric voltage in the bottom sensing PZT layer, which is in proportion to the displacement at the cantilever tip. By carefully monitoring the displacement at the cantilever tip during a given test, an accurate determination of both the force and displacement exerted on the sample surface can be ascertained, which in turn yields an accurate determination of the elastic modulus of the sample. Moreover, by placing a sensing PZT layer in the device, as shown, the maximum of the induced voltage transient of the sensing PZT can be used to accurately determine the cantilever tip displacement. The ability of the PEFS to electrically apply a force and electronically measure the displacement makes it ideal for “electronic palpation” like an “electronic finger.”

The PEFS measures the tissue compressive (shear) stiffness by touching (rubbing) the tissue surface. The force generation and displacement sensing are all within the “finger.” The PEFS may be used for in-vivo tissue imaging particularly for breast cancer and prostate cancer detection.

The PEFS can measure elastic stiffness and shear modulus of soft materials, with or without a sensing electrode. In case a sensing electrode is not used, other means such a laser or piezoelectric displacement meter can be provided for displacement determination.

EXAMPLE 1

FIG. 2( a) shows the displacement signal captured by the sensing PZT layer and by the laser displacement meter when a 10V step potential was applied to the unimorph cantilever. FIG. 2( a) shows a typical all-electrical measurement as displayed on an oscilloscope. The applied voltage (line 1), at t=0, indicates the applied voltage was turned on. Line 2 was the voltage output from the laser displacement meter for direct displacement measurements and line 3 was the induced voltage measured at the sensing PZT layer. In FIG. 2( a) the induced voltage was negative. The peak of the induced voltage was therefore at minimum near t=0. The induced voltage decayed with time due to the fact that the PZT layer was not perfectly insulating. The charge generated at the PZT surface by the cantilever bending dissipated over time. As can be seen from FIG. 2( a), the induced-voltage measurement was more sensitive than that generated by the commercial displacement meter (Keynce™ LC2450 displacemeter (Line 1)) used.

FIG. 2( b) shows the deflection signal captured by the sensing PZT layer at various applied voltages. FIG. 2( b) shows that the induced voltage increased with the applied voltage.

In FIG. 3, the peak induced piezoelectric voltage captured at the sensing electrode (open squares) and the displacement measured by a laser displacement meter (full circles), versus applied voltage, is shown. As can be seen, the peak induced voltage and the displacement are proportional to each other, validating that the displacement at the tip of the cantilever can be quantified using the peak induced voltage measured at the bottom sensing PZT layer.

EXAMPLE 2 Flat-Punch Indentation Compression Test

A flat-punch indentation compression test is a test whereby the cantilever tip is pressed on the sample surface and the cantilever contact area is much smaller than the sample surface area. This test simulates an in vivo measurement.

FIG. 4( a) is a representation of an indentation compression test on a model soft tissue using a PEFS with a sensing PZT layer, and FIG. 4( b) is a schematic of the compression indentation test. In the flat-punch indentation compression tests, the contact area, A, which was much smaller than the sample surface, was defined by gluing a thin plastic sheet of a known area on the underside of the cantilever as schematically shown in the setup depicted in FIG. 4( b). Using a traditional Hertzian indentation analysis one can relate load, displacement, contact area, and the mechanical properties of the tested material.¹⁷ When applying a voltage to the top, driving PZT layer, it generated a force, F, and caused indentation displacement, δ to the sample. The relationship between the force, F, and the displacement, δ, is described by the following expression.

$\begin{matrix} {{F = {2\sqrt{\frac{A}{\pi}}\frac{E}{1 - v^{2}}\delta}},} & (1) \end{matrix}$ wherein v is the Poisson ratio and E is the Young's modulus of the model tissue. Denoting the spring constant of the cantilever as K and the “free” displacement generated by an applied voltage V is represented as d₀, the force F exerted on the model tissue by the applied voltage V with a displacement, δ, is therefore, F=K(d₀−δ). It follows that the Young's modulus, E, is then expressed as,

$\begin{matrix} {{E_{i} = {\frac{\sqrt{\pi}}{2}\left( {1 - v^{2}} \right)\frac{K\left( {d_{0} - \delta} \right)}{\delta\sqrt{A}}}},} & (2) \end{matrix}$ wherein the subscript i of E denotes indentation.

EXAMPLE 3 Regular Compression Test

A regular compression test describes a condition where a cantilever is pressed on the sample surface and the contact area is the same as the sample surface area. A schematic of a regular compression test is shown in FIG. 5( a) where the contact area is the same as the surface area. FIG. 5( b) is a schematic of the deformation of a sample in a regular compression test under an applied voltage, V. In a regular compression test, the elastic modulus is obtained by using

$\begin{matrix} {{E_{c} = \frac{{K\left( {d_{0} - \delta} \right)}h}{A\;\delta}},} & (3) \end{matrix}$ wherein h is the height of the sample, d₀ the “free” displacement of the cantilever at voltage V, δ the displacement with the sample, K the spring constant of the cantilever and E_(c) is the elastic modulus measured by the regular compression test. For comparison, the same model tissue sample was tested using both the indentation compression and regular compression test conditions (the left-hand set of data and setup in FIG. 6( a) for regular compression and the right-hand data and setup for indentation compression in FIG. 6( b)). The elastic moduli, E_(i) and E_(c) were obtained using Eq. (2) and Eq. (3), respectively. Clearly, E_(c) obtained using Eq. (3) under the compression condition and E_(i) obtained using Eq. (2) under the indentation condition agreed with each other and also with the known value, 100 KPa, of the elastic modulus of the rubber employed for the test, thereby validating the elastic modulus measurements using both the indentation test and the compression test. These results clearly established that the elastic stiffness of tissue can be determined using flat-punch indentation tests with the piezoelectric cantilever of the present invention.

EXAMPLE 4 Tissue-stiffness Imaging by Indentation Compression

Having demonstrated that piezoelectric cantilevers are capable of determining the elastic stiffness of soft materials using the flat-punch indentation test, and that the test can be done with a driving electrode for force generation, and a sensing electrode for displacement/force detection using all-electrical measurements, here it is demonstrated that tissue elastic stiffness profiling can be done using flat-punch indentation. A simulated tissue sample with a hard inclusion was made from gelatin and candle wax. A 7 mm diameter, 5 mm tall cylinder of wax was embedded in an 8 mm thick gelatin matrix. Indentation tests were conducted at 2 mm increments over the entire surface surrounding the inclusion. The elastic modulus at each location was calculated using Eq. (2). The 2-D plot in FIG. 7( a) reflects the higher modulus values in the center, plainly evident in the corresponding contour plot (FIG. 7( b)). The image was enhanced in FIG. 7( c) through a data smoothing operation, and is seen in comparison with FIG. 7( d) to depict the approximate size and shape of the wax.

EXAMPLE 5 Dependence of Depth Limit in Detection on Probe Size

Because the indentation test only needs to press a small part of the sample surface, it is a natural configuration for in vivo application. However, because the probe size is smaller than the sample size in an indentation test, only the volume immediately beneath the indenting device is affected by the indentation test. It is thus conceivable that the detection sensitivity depends on the depth of the hard inclusion. To demonstrate this point, the effect of the probe size on the depth limit for detection using cantilevers of 3 mm width and 5 mm width was examined. Both cantilevers are 2 cm in length. The 3 mm wide cantilever had a contact area of 3 mm (the width)×2 mm and the 5 mm wide cantilever had a contact area of 5 mm (the width)×2 mm. With the 3 mm wide cantilever six wax inclusions of 7 mm diameters at varying depths beneath the top surface were embedded in a gelatin sample of 7 mm in height. For the 5 mm wide cantilever, five wax inclusions 15 mm in diameter were embedded in a gelatin sample of 18 mm in height. Cantilever indentation tests were conducted across the central axis of each sample at 1 mm increments. Elastic modulus was calculated at each location using the indentation formula, Equation (2). The result of elastic profiles of wax inclusions 7 mm in diameter embedded at different depths measured using the 3 mm wide cantilever are plotted in FIG. 8( a). Clearly, the 3 mm wide cantilever could detect the variation in the elastic modulus for depths less than 2-3 mm. When the wax inclusion was at a depth larger than 3 mm, there was no difference in the elastic modulus measured by the cantilever.

For comparison, the result of elastic profiles of wax inclusions 15 mm in diameter embedded at different depths were measured using the 5 mm wide cantilever and plotted in FIG. 8( b). With a 5 mm wide cantilever, the elastic modulus variation due to the wax inclusion could be detected at a larger depth. From FIG. 8( b), it can be seen that depth limit on the detection by a 5 mm long cantilever was about 8 mm. Comparing the elastic modulus profile results measured from the 3 mm and 5 mm cantilevers, it is clear that a wider cantilever (or wider probe) allowed detection of elastic modulus variation at a greater depth. The effect of the cantilever width on the detection depth limit is shown in FIG. 8( c).

The above results indicate that one can probe the elastic stiffness to different depths by using cantilevers having different probe sizes. Furthermore, by carefully analyzing measurements with different probe sizes, it is possible to obtain not only the stiffness variation in the lateral direction, but also in the thickness direction to thereby allow construction of 3-D tissue stiffness maps.

EXAMPLE 6 Regular Shear Test

Shear tests can be accomplished using L-shaped cantilevers. A schematic of a regular shear test is shown in FIG. 9. When a voltage was applied across the PZT, which is shown as the shaded layer in FIG. 9, it caused the cantilever to bend, which created lateral movement of the L-shaped tip and sheared the tissue sample underneath. The shear modulus can be determined using the equation:

$\begin{matrix} {{G_{c} = \frac{{K\left( {{\Delta\; x_{0}} - {\Delta\; x}} \right)}h}{A\;\Delta\; x}},} & (4) \end{matrix}$ where h and A are the height and the surface area of the sample, respectively, K is the spring constant of the cantilever, and Δx₀ and Δx the displacement of the cantilever without and with the sample, respectively.

EXAMPLE 7 Indentation Shear Test

A schematic of an indentation shear test is shown in FIG. 10. This is the most relevant condition for potential tissue shear stiffness measurement. When a voltage was applied across the PZT, it caused the cantilever to bend, which created lateral movement of the L-shaped tip and sheared the tissue sample underneath. The shear modulus can be determined using the equation:

$\begin{matrix} {{G_{i} = {\frac{\sqrt{\pi}}{2}\left( {1 - v^{2}} \right)\frac{K\left( {{\Delta\; x_{0}} - {\Delta\; x}} \right)}{\Delta\; x\sqrt{A}}}},} & (5) \end{matrix}$ wherein A is the contact area, v is the Poisson ratio, K is the spring constant of the cantilever, and Δx₀ and Δx are the displacements of the cantilever without and with the sample, respectively.

EXAMPLE 8 Comparison of all Four Measurements

For comparison of all four measurements, regular compression, indentation compression, regular shear and indentation shear, a cantilever that has a U-shaped stainless steel tip as shown in FIGS. 11( a)-11(d) was used. The advantages of such U-shaped tips include: (1) precise control of the contact area in all measurement geometry, and (2) the ability to allow the cantilever to be protected during measurements in tight spaces as illustrated by (e). The cantilever had a driving PZT layer 23 mm long, and a sensing PZT layer 10 mm long. The cantilever is 4 mm wide. Both the driving and sensing PZT layers are 127 μm thick and the stainless steel layer is 50 μm thick. The measurements were done on rubber samples with a Young's modulus of 400-500 kPa.

The results of the regular compression, indentation compression, regular shear, and indentation shear measurements on rubber samples that had a Young's modulus of 400-500 kPa using the U-shaped cantilever as shown in FIGS. 11( a)-11(d), are summarized in FIG. 12. The Young's modulus obtained from regular compression with Eq. (3) and the shear modulus obtained from regular shear measurements with Eq. (4) were 460 kPa and 148 kPa, respectively, giving a Poisson ratio of 0.5, consistent with what was expected of rubber samples. Using a Poisson ratio of 0.5, the Young's modulus and shear modulus obtained from indentation measurements with Eqs. (2) and (5) were 452 kPa and 141 kPa, respectively, in close agreement with the values obtained from the regular compression and regular shear measurements. The results shown in FIG. 12 validate the measurement of the Young's modulus using either the regular compression test or the indentation compression test, and validate the measurements of the shear modulus using either the regular shear test or indentation shear test.

EXAMPLE 9 Distinguishing Tumor Interfacial Properties by Indentation Shear Tests

Two tumor models, one with a smooth face and the other with a rough face were made of play dough and were the same size and embedded at the same depth in the model tissue gelatin as shown in FIG. 13. Both the smooth-surfaced tumor and the rough-surfaced tumor were 2 mm beneath the gelatin surface. Indentation compression and indentation shear tests were carried out on the plain gelatin surface (point A), and on the gelatin surface above the center of the smooth-surfaced tumor (point B), and above the center of the rough-surfaced tumor (point C). FIG. 14 shows the Young's modulus and shear modulus measured on plain gelatin (point A), the smooth-surfaced model tumor (B), and the rough-surfaced tumor (C) using the indentation compression and the indentation shear tests.

While both the smooth-surfaced and rough-surfaced model tumors were much stiffer than the surrounding gelatin under compression, only the rough-surfaced tumor displayed a stiffer shear. This indicates that the rough-surfaced tumor model was less mobile than the smooth-surfaced tumor model under shear. Thus, the indentation shear measurement with a piezoelectric finger was effective in probing tumor interfacial properties and tumor mobility. Combining both the compression and shear tests offers the potential of not only measuring the stiffness, but also determining the mobility of a tumor, which has great potential for tumor malignancy detection.

EXAMPLE 10 Detecting Small Satellite Tumor Missed in Preoperative Screening

The use of the PEFS in excised breast tumors has been evaluated in the laboratory. The lumpectomy specimen was from a 60-year old woman with breast cancer. The known malignancy was 1.4 cm in the largest dimension. After surgical excision, the specimen was oriented with silk sutures, scanned with ultrasound, and images were stored. The PEFS scan was performed in the same orientation to allow later correlation with the ultrasound image. The specimen was sectioned in the same orientation to allow histological confirmation of the PEFS findings as well. Using the PEFS, preliminary elastic modulus measurements were performed on breast lumpectomy samples using an 8 mm wide PEFS with a rectangular tip. FIG. 15 shows lateral elastic modulus profile of a lumpectomy sample measured by an 8 mm wide PEFS at (a) along y=0 which exhibited two tumors, a larger one at x=17-25 mm, and a smaller one at x=5-10, and at (b) along y=4 mm, which only exhibited the larger tumor at x=17-25. The dotted rectangles are meant to guide the eye. The PEFS could distinguish the cancers from the surrounding tissues.

Of note, the PEFS scan identified the known 15×13×12 mm invasive ductal carcinoma at x=15-25 mm and identified a smaller 6×5×3 mm satellite invasive ductal carcinoma at x=5-10 mm. This smaller lesion was not detected by mammogram, ultrasound or the physician's preoperative palpation.

EXAMPLE 11 Comparison of Shear Modulus to Elastic Modulus Profile of Breast Cancer

With the second lumpectomy sample (not shown), the elastic modulus, E, and shear modulus, G, profiles have been performed. The tumor was 12-10 mm in size and 5 mm below the surface. The tissue was examined with an 8 mm wide PEFS. FIG. 16 shows (a) Young's modulus (E) and shear modulus (G) profiles, and (b) G/E profile on breast tissue with cancer. The resultant elastic modulus and shear modulus profiles are shown in FIG. 16( a). Clearly both the elastic modulus and the shear modulus were much higher in the region with the tumor than in the surrounding tissue. The G/E profile is plotted in FIG. 16( b). The G/E ratio was much higher (approaching 0.6-0.7) in the tumor region than that of the surrounding tissues (around 0.3-0.4). The G/E ratio of 0.3 in the normal tissue region was expected of an isotropic material with a Poisson's ratio of 0.5.² A much higher G/E ratio in the cancer region indicated that the tumor was harder to move under shear than under compression as compared to the surrounding normal tissue. The pathological session result confirmed the malignancy.

EXAMPLE 12 Simultaneous Determination of Depth and Elastic Modulus of Tumors Using Two PEFs's of Different Widths

In FIG. 17 parts (a) and (b), are shown the lateral elastic modulus profiles of a 15 mm diameter model clay tumor in gelatin with 2.4 mm (part (a)), and 5.4 mm (part (b)) depths, as respectively measured by a 4 mm wide (the open squares) and an 8 mm wide PEFS (the open squares). The lateral location of the clay was marked by the gray shaded rectangle. Comparing the profiles obtained with 8 mm wide PEFS and those obtained by the 4 mm wide PEFS, one can see that far away from the inclusion, the values of the elastic modulus of the gelatin obtained by both PEFS's were essentially the same, indicating no inclusion underneath. Proximate to the inclusion, the values of the measured elastic moduli differed between the two PEFS' as they had different probe depths.

A separate experiment (not shown) has determined that the probe depth of a PEFS is twice the PEFS's width. With E_(gel) obtained from locations far away from the inclusion, one can then use the two profiles measured with the two PEFS' to solve the following two equations for the two unknowns, E_(inclusion) and d:

$\begin{matrix} {{\frac{d_{p,1}}{E_{{measured},1}} = {\frac{d}{E_{gel}} + \frac{d_{p,1} - d}{E_{inclusion}}}},{and}} & (6) \\ {{\frac{d_{p,2}}{E_{{measured},1}} = {\frac{d}{E_{gel}} + \frac{d_{p,2} - d}{E_{inclusion}}}},} & (7) \end{matrix}$ where d_(p,1) and d_(p,2) (E_(measured,1) and E_(measured,2)) are the probe depths of PEFS 1 and PEFS 2, respectively, E_(gel) the elastic modulus of gelatin that can be obtained from far away from the inclusion, and d and E_(inclusion) are the inclusion depth and the elastic modulus of the inclusion. Using the measured elastic modulus over the top of the center of the inclusion, the known probe depths, and the E_(gel) obtained from far away from the inclusion and solving Eqs. (6) and (7), we obtained d=2.4 mm and E_(inclusion)=109 kPa from FIG. 17 part (a) and d=5.4 mm and E_(inclusion)=102 kPa from FIG. 17 part (b). Both the deduced inclusion depths and E_(inclusion) are in agreement with the independently measured values: 2.4 mm, 5.4 mm, and 104 kPa, respectively. This clearly illustrates that lateral elastic modulus profiles measured with two PEFS' of different widths can be used to directly deduce both the inclusion depth and the inclusion elastic modulus. With more PEFS', it should be possible to obtain even more detailed axial elastic modulus profile information.

EXAMPLE 13 Direct Tumor Mobility Measurement Using Two PEFS'

In this model study, a model smooth tumor (the shaded inclusion in the back of FIG. 18) and a model rough (malignant) tumor (the white rough ball in the front of FIG. 18) were prepared. Direct tumor mobility measurement was carried out with one PEFS pushing on the side of the tumor and the other PEFS determining the movement of the tumor on the other side. With the driving PEFS pushing down 50 μm, a movement of 2 mm from the smooth inclusion and no movement from the rough inclusion were measured. This illustrated the sensitivity of the PEFS to directly measure tumor mobility for potential malignancy screening.

Preliminary measurement on breast tissues after surgery have indicated that a PEFS can detect cancerous tumors as small as 3 mm in size that were missed by mammography, ultrasound, and physician's palpation, offering great potential for early breast cancer detection. Furthermore, it was demonstrated that by using two or more PEFS's of different widths, one can simultaneously determine both the tumor elastic (shear) modulus and its depth. In addition, it has also been demonstrated that tumor mobility can be assessed by measuring the ratio of the shear modulus to the elastic modulus of a tumor, or by sensitive direct tumor mobility measurement using two PEFS's, one for pushing and one for measuring the movement. The tumor mobility measurement offers the potential for non-invasive breast cancer malignancy screening.

It is to be understood, however, that even though numerous characteristics and advantages of the present invention have been set forth in the foregoing description, together with details of the structure and function of the invention, the disclosure is illustrative only, and changes may be made in detail, especially in matters of shape, size and arrangement of parts within the principles of the invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed.

The below list of references is incorporated herein in their entirety.

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1. A sensor system comprising: a cantilever having: a first layer made of piezoelectric material enabled to provide a force; a second layer made of non-piezoelectric material; and a third layer made of piezoelectric material wherein said first layer and said third layer have different lengths; an apparatus for applying voltage via said first layer to generate a force in said cantilever; an apparatus for measuring a voltage; and a structure for transmitting an induced voltage to said apparatus for measuring a voltage, wherein the induced voltage is indicative of a displacement of said second layer resultant from said generated force, wherein said sensor is capable of simultaneously inducing a force in said cantilever and measuring a displacement of said second layer.
 2. The sensor system of claim 1, wherein said first and said second layers have different lengths.
 3. The sensor system of claim 1, wherein said first layer directly contacts said second layer and wherein said second layer directly contacts said third layer.
 4. The sensor system of claim 1, wherein said piezoelectric layer is made of lead zirconate titanate.
 5. The sensor system of claim 4, wherein said first layer directly contacts said second layer and wherein said second layer directly contacts said third layer and said first layer includes a restrained base at a proximal end thereof and a cantilever portion extending to a distal end of said first layer.
 6. The sensor system of claim 5, wherein said second layer extends beyond the distal end of said first layer to form an extended portion of said second layer.
 7. The sensor system of claim 6, wherein the extended portion of said second layer is substantially L-shaped or substantially U-shaped.
 8. The sensor system of claim 4, wherein said second layer comprises a member that extends beyond said first layer and wherein the member is oriented at an angle greater than or less than 180 degrees with respect to said first layer.
 9. The sensor system of claim 1, wherein said first layer includes a restrained base at a proximal end thereof and a cantilever portion extending to a distal end of said first layer.
 10. The sensor system of claim 9, wherein said second layer extends beyond the distal end of said first layer to form an extended portion of said second layer.
 11. The sensor system of claim 10, wherein the extended portion of said second layer is substantially L-shaped or substantially U-shaped.
 12. The sensor system of claim 1, wherein said second layer comprises a member that extends beyond said first layer and wherein the member is oriented at an angle greater than or less than 180 degrees with respect to said first layer.
 13. The sensor system of claim 12, wherein said member is oriented at a 90 degree angle with respect to a remainder of said second layer.
 14. A sensor system as claimed in claim 1 for sensing stiffness wherein said sensor system detects the stiffness of a sample by applying a force to said cantilever while said cantilever is in contact with the sample and measuring voltage from said third piezoelectric layer.
 15. The sensor system of claim 14, wherein each of said first and third layers includes a restrained base at a proximal end thereof and a cantilever portion extending to a distal end of each of said first and third layers and wherein said second layer extends beyond the distal ends of the first and third layers to form an extended portion of the second layer, and wherein the extended portion of the second layer is substantially square-shaped, substantially L-shaped, U-shaped, O-shaped, square-shaped, or tapered.
 16. The sensor system of claim 15, wherein the extended portion of the second layer is substantially square-shaped, substantially L-shaped, U-shaped, O-shaped, square-shaped, or tapered.
 17. The sensor system of claim 14, wherein said structure for transmitting an induced voltage comprises first and second electrodes located on a same side of said first layer.
 18. The sensor system of claim 14, wherein said piezoelectric layer is made of lead zirconate titanate.
 19. A sensor system comprising: a cantilever having: a first layer made of piezoelectric material enabled to provide a force; a second layer made of non-piezoelectric material; and a third layer made of piezoelectric material wherein said first layer and said third layer have different lengths and said second layer has a different length than said first layer and said third layer; an apparatus for applying voltage via said first layer to generate a force in said cantilever; an apparatus for measuring a voltage; and a structure for transmitting an induced voltage to said apparatus for measuring a voltage, wherein the induced voltage is indicative of a displacement of said second layer resultant from said generated force.
 20. The sensor system of claim 19, wherein said first layer includes a restrained base at a proximal end thereof and a cantilever portion extending to a distal end of said first layer, said second layer extends beyond the distal end of said first layer to form an extended portion of said second layer, the extended portion of said second layer is substantially L-shaped or substantially U-shaped, and said sensor system is capable of simultaneously inducing a force in said cantilever and measuring a displacement of said second layer.
 21. The sensor system of claim 19, wherein said first layer directly contacts said second layer and wherein said second layer directly contacts said third layer.
 22. The sensor system of claim 19, wherein said second layer comprises a member that extends beyond said first layer and wherein the member is oriented at an angle greater than or less than 180 degrees with respect to said first layer.
 23. The sensor system of claim 19, wherein said piezoelectric layer is made of lead zirconate titanate.
 24. A sensor system comprising: a cantilever having: a first layer made of piezoelectric material enabled to provide a force; a second layer made of non-piezoelectric material wherein said second layer comprises an exposed contact surface for contacting a sample and said exposed contact surface comprises a portion of one of an upper and lower surface of said second layer; and a third layer made of piezoelectric material wherein said first layer and said third layer have different lengths; an apparatus for applying voltage via said first layer to generate a force in said cantilever; an apparatus for measuring a voltage; and a structure for transmitting an induced voltage to said apparatus for measuring a voltage, wherein the induced voltage is indicative of a displacement of said second layer resultant from said generated force.
 25. The sensor system of claim 24, wherein said first layer directly contacts said second layer and wherein said second layer directly contacts said third layer.
 26. The sensor system of claim 24, wherein said first layer includes a restrained base at a proximal end thereof and a cantilever portion extending to a distal end of said first layer.
 27. The sensor system of claim 26, wherein said second layer extends beyond the distal end of said first layer to form an extended portion of said second layer and the extended portion of said second layer is substantially L-shaped or substantially U-shaped.
 28. The sensor system of claim 24, wherein said second layer comprises a member that extends beyond said first layer and wherein the member is oriented at an angle greater than or less than 180 degrees with respect to said first layer. 